High pressure implement hydraulic circuit

ABSTRACT

A relatively low pressure hydraulic control system for a high pressure work output system in which a control valve is selectively actuated to position a variable displacement axial piston pump to control the flow in the work output system and to position a directional valve which controls the direction of work output. In such a system wherein two work outputs are provided, thereby requiring two control valves, a priority valve may be utilized in the low pressure system so that a signal from one of the control valves will always override a signal from the other control valve in controlling the axial piston pump.

United States Patent Hufeld et al. [451 Aug. 1, 1972 54] HIGH PRESSURE IMPLEMENT [56] References Cited 72 f f: P m m J UNITED STATES PATENTS e 3,464,443 9/1969 Tennis ..l37/596.l8 x

Larson, Joliet; Howard A. Marsden, Pekin; James P. Mueller, East Peoria; William B. Norick, Joliet, all of ill.

Assigneez Caterpillar Tractor Co., Peoria, Ill.

Filed: Jan. 4, 1971 Appl. No.: 103,867

Related US. Application Data Division of Ser. No. 868,964, Oct. 21, 1969, Pat. No. 3,575,000, Continuation-impart of Ser. No. 814,003, April 7, 1969, abandoned.

US. Cl ..l37/596.l8 Int. Cl ..Fl6k 11/10 Field of Search l37/594.l4, 594.15, 594.18,

Primary Examiner-Henry T. Klinksiek Attorney-Fryer, Tjensvold, Feix, Phillips & Lempio [57] ABSTRACT .system wherein two work outputs are provided,

thereby requiring two control valves, a priority valve may be utilized in the low pressure system so that a signal from one of the control valves will always override a signal from the other control valve in controlling the axial piston pump.

3 Claims, 19 Drawing Figures ees 25I I 353 W U23 7 .345

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sum 02 0F 11 CD O) v INVENTORS JOHN L. HUFELD [U DONALD J. LARSON I HOWARD A. MARSDEN JAMES P MUELLER H WILLIAM B. NORICK PATENTED M18 I I972 sum. 03 0F 11 k E K wD Sfi TLRRLO m AE m M HJA B L D L N AE H WM O O I. IJDHJW PATENTED H973 3.680.588 sum sum 11 Elg- '5- F H l' L R I.\'\'E.\'TORS JOHN L. HUFELD DONALD J. LARSON HOWARD A. MARSDEN JAMES P. MUELLER WILLIAM B. NORICK PAIEmEDwM I912 3.880.588

sum 05 HF 11 383 I63 I79 389 I65 383 I6I 63 I79 389 I65 J 27 IAI I6I 63 79 389 INVENTDRS' 3g JOHN L. HUFELD DONALD J. LARSON HOWARD A. MARSDEN JAMES P. MUELLER WILLIAM B. NORICK P'ATEN'TEDAus' nan v SHEET 07 [1F 1 INVENTORS JOHN LHDEELD 1 DONALD J LAR HOWARD A. MARSDEN 357 JAMES P. MUELLER WILLIAM B. NORICK PATENTEDmc 1 1912 3.680.588

sum 08 0F 11' INVEN'IURS [n I JOHN L. HUFELD 4 DONALD J, LARSON HOWARD A. MARSDEN JAMES P MUELLER IQ] WILLlAM 8. NORICK PAIENTEM: H972 3.680.588

sum 09 HF 11 P1 J E INVENTORS JOHN L. HUFELD DONALD J. LARSON HOWARD A. MARSDEN JAMES P. MUELLER WILLIAM B. NORlCK PATENTEmus H972 3.880.588

SHEET 10 [IF 11 I56 I60 I54 94 /(Z98)- 99 r152 (33]) M48 INVENTORS JOHN L. HUF'ELD DONALD J. LARSON HOWARD A. MARSDEN JAMES P. MUELLER WILLIAM B. NORICK mtmemuc' m 3,680,588

I sum 11 [1F 11 I I I l I v m \"EN TOR JOHN L HUEELD DONALD Jv LARSON HOWARD A, MARSDE N JAMES F? MUELLER VVILLFAM B NORICK HIGH PRESSURE IMPLEMENT HYDRAULIC CIRCUIT This application is a division of application Ser. No. 868,964, filed Oct. 21, 1969, now U. S. Pat. No. 3,575,000, which in turn is a continuation-in-part of application Ser. No. 814,003, filed Apr. 7, 1969 and now abandoned.

BACKGROUND AND SUMMARY OF THE INVENTION As hydraulically controlled machinery becomes larger and more complex, the component parts used in controlling such machinery, such as cylinders, connecting lines, and valves, must be increased in size so as to withstand the high pressure forces which are developed both by the control system itself and by reaction forces from the work. With increased flow and higher pressures, leakage within directional valves which utilize cylindrical spools has become a problem and the costs of manufacture of such valves has greatly increased due to the close tolarances which must be maintained.

If the control systems are simply increased in size and the supply of fluid comparably increased, the excess flow must be throttled back to the tank or reservoir during times when all the flow is not desired to perform a particular function. The excess flow is converted to heat and wasted in the throttling process. Similarly, when the machinery is stalled, much energy is again wasted.

in machinery having articulated movement, it is quite desirable to reduce the number of large high pressure lines that are required to pass over the swivel joints. For this reason, directly operated control valves are not suitable for use on the large articulated machines since the valves would have to be mounted close to the operators station, requiring a considerable number of high pressure hoses to pass over swivel joints.

The high pressure implement hydraulic control system of the present invention utilizes a variable displacement, axial piston-type pump that is capable of producing the increased flows and pressures that are necessary to operate large modern machinery. Although any desired machinery may be so operated, the system is especially adaptable to articulated machinery since it obviates the problem of high pressure lines passing over swivel joints.

Essentially, the invention involves the use of a high pressure machinery actuating circuit which is operated and controlled by a low pressure control circuit.

With this system, the operator can limit the flow necessary to perform a particular function reducing heat and energy losses thereby making the system more efficient. Additionally, the control of pump displacement allows the utilization of directional valves having poppet-type spools, since the throttling is not done by the spools. Use of the poppet-type spools provides positive leakage control and decreases overall manufacturing costs of the directional valve packages. Precise control of the directional valve is achieved by the use of pilot-operated, vented check valve arrangements to control the actions of the poppet-type spools, and is synchronized with the rest of the pilot system so that the directional valves will function at the proper times.

Should the machinery become stalled, the pump is automatically adjusted to a low delivery rate while maintaining the same pressure or cylinder force, causing a reduction in heat and energy loss. in such a case, the engine power demand is also substantially reduced.

To reduce the number of high pressure lines crossing the swivel joints, the main control valves will be mounted close to the components they control and will be actuated by the low pressure, pilot system. The displacement of the variable displacement pump is also controlled by the pilot system and the control of the displacement and directional valve is synchronized so that the proper amount of supply fluid and pressure is available at all times.

It is therefore an object of this invention to provide a hydraulic system wherein the pressure and direction of flow in a high pressure circuit are controlled by a low pressure circuit.

It is also an object of this invention to provide a hydraulic circuit which may be used to control an articulated machine while not requiring a large number of high pressure lines to pass over the machine's swivel joints.

It is also an object of this invention to provide a high pressure machinery actuating circuit which is operated and controlled by a low pressure control circuit.

It is a further object of this invention to provide a hydraulic system capable of producing the high pres sures required by todays machinery while maintaining a high degree of efficiency by constantly controlling the fluid flow in the system.

It is also an object of this invention to control the high pressure fluid flow in such a system by means of a low pressure actuated, variable displacement, axial piston-type pump.

It is also an object of this invention to provide a hydraulic circuit having high efficiency due to the reduction of heat and energy losses through the control of hydraulic flow necessary to perform a particular function.

It is a further object of this invention to provide a hydraulic circuit utilizing directional valves having poppet-type spools.

It is a further object of this invention to provide in such a circuit a system which produces positive leakage control while decreasing overall manufacturing costs of the directional valves.

It is a still further object of this invention to provide, in such a circuit, precise directional valve control through the use of pilot-operated, vented check valve arrangement to control the actions of poppet-type spools.

It is also an object of this invention to provide such a circuit wherein, when the machine is stalled, automatic adjustment to the circuit occurs to allow a low fluid delivery rate while maintaining a constant pressure.

Other objects of the invention will become apparent to those skilled in the art upon perusal of the following description in light of the accompanying drawings which illustrate preferred embodiments of the invention. Embodiments using similar or equivalent structure, which are included in the scope of the appended claims, will become obvious to those skilled in the art without departing from the present invention as defined in the appended claims.

BRIEF DESCRIPTION OF THE DRAWINGS the high pressure implement hydraulic circuit of the instant invention;

FIGS. 3-6 illustrate schematic sectional views of an operator-actuated control valve utilized in the subject hydraulic circuit, with the valve spool in various positions of actuation;

FIGS. 7-9 illustrate schematic sectional views of a priority valve which may be utilized in the subject circuit with the valve spool subjected to varying degrees of actuation;

FIGS. 10 and 11 illustrate schematic sectional views of a pilot valve in the subject hydraulic circuit, with the valve spool in unactuated and fully actuated positions respectively;

FIG. 12 illustrates a schematic sectional view of a servo valve in the subject circuit;

FIG. 13 illustrates a schematic sectional view of a sequence valve used in the control circuit; and

FIG. 14 is a sectional schematic illustration of a directional valve in the subject circuit; I

FIG. 15 is a schematic view of a modified embodiment of that portion of the invention shown in FIG. 2;

FIG. 16 is a sectional schematic illustration of a modified embodiment of the directional valve shown in FIG. 14, utilized in the circuit of FIG. 15;

FIGS. 17 and 18 are modified embodiments of the valvesillustrated in FIGS. 10 and 11, which may be utilized in the circuit shown in FIG. 15; and- FIG. 19 is a sectional schematic illustration of a modified embodiment of the directional valve shown in FIG. 16 which may be utilized in the circuit of FIG. 15

i with slight modification thereof.

DETAILED DESCRIPTION The following description relates to the use of a high pressure implement hydraulic circuit in any desired application. For ease in illustration,however, the description will refer to the use of the circuit on large loaders wherein lift and tilt circuits will be designed to utilize maximum pressures up to about 6,000 psi. Many modifications of the circuit, including deletion and duplication of elements, will be obvious to those skilled in the art when using the circuit for other applications.

It should be noted that the lift and tilt circuits in the system are, in many respects, duplicate circuits. Therefore, the following description will be essentially directed toward the lift circuit upon the understanding that similar actions cause similar results in the tilt circuit. Of course, where distinctions do exist between the circuits, they will be fully discussed.

Now referring to the schematic illustration of the circuit shown in FIGS. 1 and 2 together, a charging pump 21 drawing fluid from a reservoir or tank 23 passes the fluid through a line 25, a steering valve 27, a cooler 29, a filter 31, and lines 33 and 35 to a variable displacement, axial piston-type pump 37.

When steering control valve 27 is actuated by the operator, fluid is directed from pump 21 to the steering cylinders (not shown) and back again through lines 39 and 41 so that the flow to pump 37 is not interrupted whenthe vehicle is being steered.

When pump 37 is in a neutral position, it requires very little flow or pressure through line 35. In such a condition of operation, the fluid in line 33 passes into line 43 and through a bypass check valve 45 which allows the flow to bypass the pump and pass into the main supply manifold 47. With the lift and tilt circuits, which will be more fully described below, in hold positions, fluid in line 47 will pass through a sequence valve 49, lines 51 and 53, sequence valve 55, line 57, and back to the tank 23.

Although the pressure of the fluid delivered by pump 21 to line 33 is normally governed by a relief valve 59, when pump 37 is in the neutral condition previously described, the pressure in line 33 is dictated only by line losses, thus reducing horsepower loss while maintaining full supply lines.

When either the lift or the tilt circuit is actuated, causing pump 37 to be stroked, pressure in line 47 will close check valve 45, and that portion of the charging flow not needed to supply pump 37 will be returned to tank 23 through relief valve 59.

A control pump 61 also draws hydraulic fluid from tank 23 for actuation of the various control valves in the implement hydraulic circuit. Fluid from the control pump is delivered through a line 63 and a filter 65 to an accumulator charging valve 67. The fluid is then directed through the charging valve into a line 69 which delivers the fluid to a pair of closed-center control valves 71 and 73. The fluid in line 69 is also delivered to a linear servo valve'75 through a line 77 and is then directed to an actuating cylinder 79, when the servo valve is shifted in either one of two operating directions. A relief valve 81 maintains a maximum pressure of about 625 psi in the lines 69 and 77 6 Pump 61 also supplies fluid to the accumulator and brake circuit, when needed, through a line 83.

As previously stated, it will be assumed that the invention is being applied to a loader having a lift circuit which is controlled by valve 71 anda tilt circuit which is controlled by valve 73. I

In FIGS. 3-6, there are illustrated schematic 'sec-' RAISE When the operator wishes to raise the loader bucket, he actuates the spool 85 to the position shown in FIG. 4

and labeled R in FIGS. 1 and 3 by means of any;

suitable linkage (not shown). Control fluid, maintained at 625 psi, is available to valve 71 through line 69,

wherein it is directed to annuli 87 and 89 by a passage 91. Movement of the spool 85 to the R raise position overcomes the force exerted by a centering spring 93. This causes pressurized fluid in annulus 89 to be communicated to an annulus 95, viaan annular groove 97,

and then into a line 99 via passage 121. The pressure in line 99 can be controlled by the operator between the limits of 0 and 625 psi by means of variable area throt-- tling slots 123 between land 125 and annular groove 97 on the spool 85. The pressure in line 99 increases as the spool is moved to the right, and when spool 85 is in the position shown in FIG. 4, i.e., its fully shifted position, control pressure in line 99 is 625 psi.

As will be explained later, the pressure in line 99 will be used to properly sequence the other control valves when it is in a range from 0 to 300 psi. When it is between 300 and 625 psi, it is used to stroke the linear servo valve 75, thereby creating an implement pump flow proportional to the control pressure, i.e., 300-625 ps1.

Thus the operator has the ability to actuate the lift cylinder at any velocity he desires. Since valves 71 and 73 are essentially identical, it can be seen that the operator also has the ability to actuate the tilt cylinder at any desired velocity.

When the spool 85 is in the extreme raise position, as shown in FIG. 4, a plunger 127 is forced into a detent groove 129 by a spring 131. This action will cause the spool to be maintained in that position either until a signal is received by valve 71 in a manner to be explained later, or until the operator manually actuates the spool 85, causing the plunger to ride up the sides and out of the groove. Thus the operator is relived of the necessity of holding the control lever in the raise position during that portion of the work cycle.

Referring again to FIGS. 1 and 2, line 99 directs the pressurized fluid from valve 71 to a shuttle valve 133 which is shifted by the fluid so that the fluid is directed through a line 139 to a priority valve 141 which will be described later.

The fluid in line 99 is also directed to a line 135 leading to a kick-out valve (not shown), mounted on the lift cylinder, and to a pilot valve 137.

Referring to FIGS. and 11, fluid from line 99 enters a chamber 143 in valve 137 and the force of the pressurized fluid works against the end of a spool 145 to move the spool to the right, against a force developed by a spring 147, to a maximum position as shown in FIG. 11. The pre-load on spring 147 is such that the spool 145 will attain the position shown in FIG. 1 1 when the pressure in chamber 143 reaches 150 psi.

As spool 145 moves to the right, pressure in a line 149, which is the same as the pressure in line 53, (see FIG. 2) will be directed from an annulus 151 to an annulus 153, via an annular groove 155, into a passage 157, and then to line 159 for a purpose to be described later.

With respect to priority valve 141, FIGS. 7-9, the line 139 directs the pressurized fluid to an annulus 161 via a passage 163 to which a passage 165 is interconnected. As the manipulation of spool 85 in valve 71 provides an increase in pressure in line 139, that pressure is also sensed in a chamber 167 in the valve 141, via passage 165. The force in chamber 167 acts upon a piston 169 which, in turn, acts on a piston 171 and a spool 173, to move the pistons and the spool against a force exerted by a spring 175, to the position shown in FIG. 8. When control pressure in line 139 reaches approximately 200 psi, the position of the pistons and spool as shown in FIG. 8 will be attained, and even through the signal pressure increases to 625 psi, the spool 173 will not move further to the left because of the small reaction area of piston 169 as opposed to the additional force of a spring 177 against which the slidable assembly now abuts. At that time, pressurized fluid in annulus 161 will be in communication with an annulus 179 via annular groove 181. This fluid is then directed to a line 183 via a passage 185.

The line 183 directs the fluid to the linear servo valve as shown in FIGS. 1 and 12. The fluid is directed into a chamber 187 wherein it works against a piston area 189 on a reciprocable spool 191 located in the valve 75, to move the spool against a force developed by a spring 193.

As this occurs the previously mentioned pressurized fluid in line 77 enters an annular groove 195 and is communicated to a line 197 by the annular groove. As shown in FIG. 1, the line 197 communicates with the actuating cylinder 79, and introduction of pressurized fluid into the head end of the cylinder will cause the cylinder housing 221 to move upwardly since the rod 223 is pivotably secured to the vehicle frame. Since the housing 221 is pinned to the body ofpump 37, an upward movement of he housing imparts an upward movement to the pump. As the fluid enters the head end of cylinder 79 through line 197, fluid is expelled from the rod end of the cylinder through line 431. When the fluid enters valve 75 through line 431, it enters an annular groove 212 around the sleeve 191 which connects with a drain line 214 so as to return the fluid to tank 23.

Since the body of valve 75 is fastened to pump 37 and a rod 225 of the valve is fastened to the vehicle frame, the resultant upward movement of the body of valve 75, relative to the spool 191 therein, will close off the supply of pressurized fluid from line 77 to line 197, thereby cutting off flow of fluid to cylinder 79 and stopping the rotation of the pump 37 at its desired displacement position. Thus, the pump delivers oil flow to the line 47 in proportion to the pressure of the fluid in line 183.

When priority valve 141 is returned to a neutral position so that pressure is released from line 183, the force of spring 193 will move sleeve 191 downwardly so that line 197 is connected to passages 214 which are in communication with an enlarged inner diameter 216 in sleeve 191. The enlarged inner diameter is in communication with the annular groove 212 by means of a passage 218. This allows fluid in the head end of the actuating cylinder 79 to be expelled to tank 23 since pressure in line 77 will be directed to the rod end of the actuating cylinder via annular groove 195, passage 429, and line 431. This will effectively swivel the pump 37 back to its minimum displacement position.

Referring once again to the pilot actuated valve 137 (FIGS. 10 and 11), when the valve is actuated to the position shown in FIG. 11, the pressure in line 159 will set a shuttle valve 227 (FIG. 2) to communicate the fluid from line 149 to a line 229 which, in turn, communicates with a main directional control valve 231, the operation of which will be described later. The fluid in line 229 also connects with a shuttle valve 233 which is shifted so that the fluid from line 229 is communicated to a line 235 which is connected to the sequence valve 55.

Referring now to FIG. 13, it can be seen that fluid entering the sequence valve through line 235 acts against a poppet 237 and the combined pressure of the fluid and the force of a biasing spring 239 serve to set the poppet so as to block the flow of fluid from line 53 to return line 57. This allows pressure to build up in line 53, as required, up to a maximum of approximately 6,000 psi as determined by the setting of a relief valve 241 (FIG. 1).

As shown in FIGS. 2 and 11, movement of the spool 145 of valve 137 to the position shown in FIG. 11 will also open a line 243 to tank 23 via a line 245. The opening of line 243 to tank will aid in the conditioning of valve 231 for operation as described below.

A sectional schematic view of the main control valve 231 is shown in FIG. 14. Since the valve is a directional-type valve, all of the components that are in the lower half of a figure are identical to and function in a manner similar to the components shown in the upper half.

As described above, the line 243 will be fully open to tank when the spool 145 in pilot valve 137 is fully shifted. When this occurs, a combination of force from a spring 247 and hydraulic force from fluid in chamber 249 will move a piston 251 away from a poppet valve 253 and the poppet will function as a load check valve. The hydraulic fluid in chamber 249 enters the chamber via orifices 255 in the poppet and is communicated to the orifices via a chamber 257 and line 259 connecting the chamber to the head end of a lift cylinder 261. The hydraulic pressure exerted by this fluid is created by the normal load reaction forces exerted by the bucket on the lift cylinder 261. Thus, the pressure in chamber 249 forces piston 251 away from the poppet 253, but also serves to hold the poppet against its seat.

-As the operator strokes the control valve 71 so that a control pressure of at least 300 psi is reached, the pump 37 provides a flow through lines 47and 53. As a result, a'build-up of fluid pressure in line 53 and passage 263 occures. When this pressure raises to a level slightly higher than the load reaction pressure in passage'257, poppet 253 will move upwardly and allow a flow of fluid from passage 263to passage 257, which fluid is then directed to the head end of thelift cylinder 261 via line 259. r

During this operation, no fluid in passage 263 can move past poppet 265 for a reason which will become obvious later.

Also during this time, a check valve spool 267 will be maintained againstits seat by the combined force of a spring 269 and fluid under pressure in chamber 271. The fluid pressure in chamber 271 is gained by fluid entering the chamber from passage 257 via an orifice 273 in the head of the spool. Since the fluid in chamber 271 will act upon an area of the spool equal to the area against which the fluid in chamber 257 will act, the spring 269 will normally cause the check valve spool to be retained against its seat. The pressure in chambers 257 and 271' will be blocked from tank by a poppettype relief valve 275, which will be maintained against .118 seat by the force exerted by a spring 277, unless the pressure in chamber 271 exceeds the pressure setting predetermined by the spring 277.

The flow of high pressure fluid through line 259 and into the head end of lift cylinder 261 will cause fluid to be expelled from the rod end of the cylinder into a line 279. The line 279 communicates with a chamber 281 in the bottom half of valve 231.

, As previously stated, line 229 is connected to line 53 through the pilot valve 137 connection of lines 159 and 149. Therefore, pressure developed by the pump 37 will be exerted in a chamber 283 in valve 231 and will work against a piston 285, moving it to the right against force developed by a spring 287. This relieves the preload on a spring 289 and thereby relieves a poppet valve 291, allowing the fluid flowing into chamber 281 from line 279 to pass into tank 23 via a line 293. This occurs since the relief of the poppet-type relief valve al-- lows the unseating of a check valve 295, similar to valve 267, in the lower half of the directional valve 231. Should cylinder 261 attempt to run faster than that velocity dictated by the pressure flow of pump 37, the pressure in line 53 decreases since the pump is not actuated to an amount required for that movement. When this pressure decreases to about 200 psi, the force of spring 287 overcomes the hydraulic force in chamber 283, and piston 285 moves to the left, setting the poppet-type valve 291, so that the lower check valve 295 reseats and restricts the flow of fluid exiting through line 293. Pump pressure will then build up to a level required to position piston 285 so that the check valve 295 meters a flow rate out of cylinder 261 equal to the pump input of the cylinder.

Throughout the above sequence of events, pressure in line 149 is provided through a spool in a pilot valve 297 to a line 299. Valve 297 is similar to valve 137and,= during this time, the spool in valve 297 is in the position shown in FIG. 10. This causes piston 321 to set poppettype valve 265 (FIG. 14) so as to prohibit flow of fluid from passage 263 into passage 281 since the area of piston 321 is large enough that the pressure in passage 263 cannot overcome it due to the smaller area of valve 265. Thus, fluid in passage 263 cannot move into chamber 281. 7

As mentioned previously, fluidunder pressure inline 99 is communicated to a line 135 'which delivers the fluid to a kick-out valve of conventional design mounted on the lift cylinder. When the lift cylinder reaches its maximum stroke, a cam will open a spool in the kick-out valve so that flow is providedto an annular chamber 323 (FIG. 4) around spool of valve 71 from a line 325. Pressure will build in chamber 323 due to the orifice 323a in the drain passage of the valve 71, to counteract the force from spring 131 and retract plunger 127, allowing the force of spring 93 to return the spool 85 to the neutral position, thereby stopping the raise cycle.

ALTERNATE EMBODIMENT The total hydraulic circuitry for the alternate embodiment can be seen by separating FIGS. 7 l and 2 and placing FIGS. 1 and 15 in a similar end-for-end position. The valves illustrated in FIGS. 16-18 are those utilized in the alternate embodiment.

When it is desired to put the machine of the altemate' embodiment in the raised mode, valve 71 is actuated in the manner previously described, with identical results relative to line pressurization, priority valve actuation, etc. Pilot flow from line 69 is directed to line 99 which connects with shuttle valve 133 to direct pilot fluid to the valve 141 and to a second stage pilot valve 138 which replaces the previously described valve 137. Valve 138 is shown in cross-section in FIGS. 17 and 18 in the unactuated and fully, actuated positions respectively. Pilot pressure in line 99 will shift the valve 138 so that pump pressure in line 149 will be directed to a line 158 via an annulus 154, an annular groove 156 around spool 146, and annulus 160, since spool 146 is shifted to the right against force from spring 148, as shown in FIG. 18.

With line 158 at pump pressure from line 149, the shuttle valve 228 will be shifted so that line 158 is communicated with a line 230. The line 230 communicates with the modified directional control valve 232 and a shuttle valve 234. When line 230 is pressurized, shuttle valve 234 is shifted so that line 230 will be connected to a line 236 to set the sequence valve 55 for proper operation of the directional valve 232.

The modified directional control valve 232 is shown in detail in FIG. 16, and pressurization of line 230 will condition the valve for actuation of lift cylinder 261 as follows:

A check valve spool 254 is moved to the right against a force from a spring 248 so that pump fluid under pressure from line 53 and passage 264 can get into passage 258, via an annular groove 256 around spool 254 and a chamber 250 containing the spring 248. Fluid under pressure in chamber 258 will be directed to a chamber 272, through an orifice 274, so that pressure can aid the force of a spring 270 in blocking a check valve 268 in the closed position. Thus, fluid in passage 258 will be directed to lift cylinder 261 via a line 260.

The poppet-type relief valve, shown generally at 276, will protect the circuit from any over-pressure conditions in that when a predetermined pressure is reached, it will open and vent the spring chamber 272 to tank through passage 252 and line 252a.

Since spool 350 will not be under the influence of a pilot pressure, the spring 352 will keep it in the position shown in FIG. 16 to prevent communication between passage 252 and a line 252b.

Pressurization in line 230 is also directed to a chamber 284 and will move a spool 286 upwardly against force from a spring 288, Upward movement of the spool 286 will connect a passage 322 to tank line 252b via an annular groove 286a around spool 286. This will cause the chamber behind the load check valve 296 to be at tank pressure so that the load check valve can be opened, thereby connecting line 280 to the tank line 294 via a passage 282 and an annulus 282a. Thus, fluid can be expelled from the rod-end of the lift cylinder 261 during the raise mode when pump fluid is directed to the head end of the cylinder as described above.

LOWER When the operator wishes to lower the loader bucket, he actuates the spool 85 to the position shown in FIG. and labeled L in FIGS. 1 and 3, overcoming the centering force of spring 93.

The 625 psi control fluid available to valve 71 through line 69 is again directed to annuli 87 and 89 via passage 91. The pressurized fluid in annulus 89 is blocked by land 125 on the spool 85; on the other hand, the fluid in annulus 87 is delivered to an annulus 327 via an annular groove 329. The fluid is then passed into a line 331 through passage 333. The pressure in line 331 can be controlled by the operator between the limits of 0 and 625 psi by means of variable area throttling slots 335 between land 337 and annular groove 329 on the spool. The pressure in line 331 increases as the spool is moved to the left, and when spool is in the position shown in FIG. 5, control pressure in line 331 is 625 psi.

When the control pressure in line 331 is in a range from 0 to 300 psi, it is used to properly sequence the other control valves and when it is between 300 and 625 psi, it is used to stroke the linear servo valve 75, thereby creating an implement pump flow proportional to the controlled pressure, i.e., 300-625 psi.

Thus the operator has the ability to lower the loader bucket at any velocity he desires.

Referring again to FIGS. 1 and 2, line 331 directs the pressurized fluid from valve 71 to shuttle valve 133 which is shifted by the fluid so that the fluid is directed to line 139 and priority valve 141. The priority valve is actuated by the control fluid in the same manner as previously described for the raise mode, relative to FIG. 8.

The fluid in line 331 is also directed to a pilot valve 297 which is identical in construction to the pilot valve 137 which was previously described. As shown in FIGS. 10 and 11, the line reference numerals in parentheses refer to those lines leading to and from valve 297 which are distinct from the lines leading to and from valve 137. Since the interior structure of the valves are identical, however, the same reference numerals are used in the following discussion wherever possible. Similar use of parentheses will be used relative to FIGS. 17 and 18 when describing the alternate embodiment.

Fluid from line 331 enters chamber 143, in valve 297, and the force of the pressurized fluid works against the end of spool 145, moving the spool to the right against the force developed by spring 147, to the position shown in FIG. 1 1. The preload on spring 147 is such that the spool will attain the position shown in FIG. 11 when the pressure in chamber 143 reaches psi.

As spool 145 of valve 297 moves to the right, pressure in line 149 (which is the same as pressure in line 53) will be directed from an annulus 151 to an annulus 153 via an annular groove 155, into a passage 157, and then to a line 339.

The fluid in line 339 sets a shuttle valve 341 which then directs the fluid to a line 343. Fluid passing through line 343 then sets shuttle valve 233 and, passing through line 235, sets sequence valve 55 in the manner previously described relative to FIG. 13. Additionally, the fluid in line 343 passes through line 345 to a chamber 347 in control valve 231 (FIG. 14) where it serves to actuate a piston 349 against the biasing force of a spring 351, thereby relieving poppet valve 275. This allows fluid flowing into chamber 257 from line 259 and the head end of lift cylinder 261 to pass into tank 23 via a line 353. This occurs since the relief of the poppet-type relief valve 275 allows the unseating of check valve 267.

As shown in FIGS. 2 and 11, movement of the spool 145 of valve 297 to the position shown in FIG. 11 will open line 299 to tank 23 via a line 355. Since valve 137 is in he unactuated position shown in FIG. 10, line 149 provides pressure to a line 243 through the valve so that load check valve 253 in the main directional control valve 231, is maintained in the closed position. 0n the other hand, since line 299 is vented to the tank through valve 297, which is in the position shown in FIG. 11, load check valve 265 of the directional valve allows fluid in chamber 263 to pass into chamber 281 and the rod end of lift cylinder 261 via line 279.

In other words, when the operator places spool 85 of control valve 71 in the lower position, fluid passes through the main directional control valve 231 in the opposite direction to that which occurs when spool 85 is placed in the raise position.

ALTERNATE EMBODIMENT With reference to FIGS. 1 and 18, when the valve 71 is shifted to the L or lower position, the second stage pilot valve 298 will be activated, causing pressure in line 149 to be transmitted to a line 340 to shift a shuttle valve 342. This connects line 340 with a line 344 which, in turn, connects with a line 300, a line 346, and shuttle valve 234. i

As shown in FIG. 16, the line 300 will direct pressure so as to shift a check valve spool 266 which is identical to the spool 254. Pressure in line 346 will be directed to a chamber 348 to move spool 350 downwardly to vent the chamber behind the load check valve 268. Due to these events, pump flow from line 53 will be directed to passage 282 and since that passage will be blocked from the line 294 by load check valve 296 in a manner similar to the way that load check valve 268 blocked line 354 in the raise mode, pump fluid will be directed to the lift cylinder 261 via line 2 Movement of spool 350 downwardly, due to the flow in line 346, causes passage 252 to be vented to line 252b, and thereby to tank 23, to unload the check valve 268 and permit fluid being expelled fromlift cylinder 261 to be returned to tank via line 260, passage 258, andaline 354.

FLOAT When the operator moves the control spool 85 of valve 71 to the float position shown in FIG. 6 and labeled F in FIGS. 1 and 3, the bucket is allowed to move up or down as externalforces dictate and flow from lift cylinder 261 can pass to and from tank 23 as needed.

With'the control spool in the position shown in FIG. 6, line 69 is connected to a line 357 via annuli 89 and 361 and annular groove 363. Thus, a control signal of 625 psi is sent to shuttle valves 341 and 227, setting the shuttle valves and passing the fluid to lines 229 and 343, thereby causing relief of poppet-type relief valves 275 and 291 and setting of sequence valve 55, all in the previously described manner.

Line 69 is also connected, via passage 91, annulus 87, groove 329, annulus 327, and passage 333 to line 331. As previously described, the fluid in line 331 actuates priority valve 141 to create a flow in line 53 and also actuates pilot valve 297 to connect line 299 to tank, thereby releasing piston 321 so as to allow valve 265 (in valve 321) to act as a check valve.

Since load check valve 253 is held closed because pilot valve 137 is not actuated and since sequence valve 55 is closed and poppet valve 291 is relieved as described, the flow in line 53.will pass load check valve 265 and valve 295 and return to tank via line 293. Since the flow in line 53 is returning to tank, the fluid passing from line 149 to 339 through valve 297 will not have great enough pressure to effect the setting of shuttle valve 341.

With the hydraulic system set in this manner, it can I readily be seen that the system will allow a true "float" of the bucket but is in a condition to allow immediate force application to lift cylinder 261 when the operator ALTERNATE EMBODIMENT Once again with respect to the alternate embodiment, in FIG. 17, with the valve 138 in its neutral position, the annulus is connected to a tank line 246 via an annulus 152 and the annular groove 156. Therefore, line 158 will be at tank pressure so that the shuttle valve 228 (FIG. 15) can be shifted to condition the circuitry for the float mode. When valve 71 is shifted to the float position, pilot pressure from line 69 is directed to line 357 and will shift shuttle valves 228 and 342 so that lines 230 and 346 will be pressurized. This has the effect of unloading both the valves 268 and 296 to permit free flow of fluid within the directional control valve and allow the lift cylinder 261 to let the bucket drop to the ground by gravitational force alone.

' TILT CIRCUIT With respect to the tilt circuit, it should be noted that the dump and rack back modes, labeled D and RB (FIG. 1), as controlled by valve 73, are identical to and operate in the same manner as the raise and lower modes as controlled by valve 71, withthe exception that flow through the sequence valve 49 does not return to tank but instead communicates to line 53 as shown in FIG. 2. Also, fluid flow from the lower half of directional valve 369, in the tilt circuit, is directed to line 53 via a line 371 and a check valve 373. The checkvalve 373 prevents high pressure fluid from flowing back into the low pressure side of the directional valve 369. This allows activation of the lift system when the vehicle bucket is being dumped. When the bucket is being racked back, the upper half of valve 369 will be the load pressure side of the valve and fluid returning from the tilt cylinder 375 will go directly to tank via line 377 and will not be available to the lift system. Consequently activation of the lift system is interrupted during the rack back portion of the work cycle.

In priority valve 141, during a tilt operatiompressure from the tilt control valve 73 is directed through a line 379, a shuttle valve 381 and a line 383 to an annulus 385 via a passage 387 in valve 141. Control pressure in passage 387 is also directed through a passage 389 to a chamber 391 wherein it acts againstpiston 171 to drive spool 173 to the extreme left position shown in FIG. 9 against the forces of springs 175 and 177. The piston 171 is sized such that, at a control pressure of 300 psi in line 383, the spool 173 is shifted to the FIG. 9 position.

The control signal is then supplied through annulus,

385, annular groove 393, annulus 395, passage 185, and line 183 to the linear servo valve 75 for control of the displacement of pump 37.

Thus it can be seen that the tilt signal will override the lift signal. For example, if the lift control valve is calling for maximum pressure in line 139, 625 psi will be urging piston 169 to the left. However, the force available against the smaller piston is inadequate to move the spool 173 past the position shown in FIG. 8. If the tilt control valve is also actuated, the tilt signal causes the spool to be moved to the position shown in FIG. 9 by the time it reaches 300 psi, causing an interruption of the lift signal from line 139. The tilt control signal is now supplied to the linear servo valve 75 and the displacement of the pump can be further increased to supply both the lift and tilt circuits adequately.

If the maximum pressure output of pump 37 should ever exceed 6,000 psi, a pilot-operated relief valve 241 will automatically activate to relieve that pressure. In so doing, some of the relieved flow will pass through the pilot portion of the valve and through a line 397 back to tank 23. However, a small orifice 399 restricts the flow through line 397 enough to produce a pressure in a line 421 which communicates with the priority valve 141. Fluid under pressure in line 421 is communicated to chamber 423 in the priority valve and the combined force resulting from this pressure in chamber 423 and the biasing force of springs 175 and 177 is large enough to overcome the force being developed in either chamber 167 or 391, so that the spool 173 will be moved back toward the neutral position.

In that event, pressure in line 183 is communicated to tank via passage 185, annulus 179, annular groove 181, annulus 425, and a line 427. This will cause the pressure in chamber 187 of servo valve 75 to reduce to tank pressure and allow force from the spring 193 to move spool 191 downwardly, communicating annuli 195 and 429 so as to transfer fluid from line 77 to line 431 and force pump 37 to return to the zero displacement position. This assures that parts and components will not be damaged during the overpressure condition and that over-heating will not occur.

ALTERNATE EMBODIMENT It is felt that the description of the original embodiment, together with the description of the alternate embodiment for the three operational modes, will cause the operation of the machine utilizing the alternate embodiment to be obvious.

MODIFIED ALTERNATE EMBODIMENT The modified alternate embodiment of FIG. 19 is essentially identical with that illustrated in FIG. 16; therefore, wherever possible, identical identification labels have been utilized. Except as explained below, the operation of the two valves is the same. The distinctions between the two directional valves occur primarily with respect to the structure and operation of the load check valves 268 and 296.

Under certain conditions of operation, it may prove to be desirable to provide greater stability in the operation of the check valves 268 and 296. This can efiectively be accomplished by eliminating the apertures 274 (FIG. 16) from the valves, and installing inserts 411 and 413 (FIG. 19) in the compartments 252 and 322, respectively. Insert 411 may be provided with an aperture 415 which communicates with passage 258 via a line 417 which is connected to line 260 in the manner illustrated. Similarly, an aperture 419 and insert 413 communicates with passage 282 via a line 421 which is connected to line'280.

Referring to the upper half of the valve for example, the pressure in passage 258 is communicated to chamber 272 via line 260, line 417, aperture 415, and passage 252. When the pressure in passage 258, and therefore passage 252, reaches a predetermined level, the poppet relief valve 276 will be opened so that the passage 252 and the chamber 272 will be connected to tank. This will allow pressure in passage 258 to work against the face of the check valve 268 and move it from its seat so that the passage 258 can be opened to tank 23 via line 354.

When the head end of the cylinder 261 is thus relieved, and it is desired to maintain a controlled flow of fluid from the passage 258 to the line 354, the valve spool 350 will be moved downwardly against the force of spring 352 by pressure exerted through line 346 in response to manipulation of the main control valve. When the spool 350 is shifted, fluid flows from line 417 around an annular groove on the spool, past a land 350a, and into the line 252b. A pressure drop in passage 272 will occur as a result of this connection, allowing the valve 268 to unseat. This pressure drop is modulatable by adjustment of the position of land 350a. Further movement of the spool 350 will cause the effect of the pressure drop on check valve 268 to change from the control of land 350a to land 350b, which influences flow from line 417 to the annular groove.

Flow check valve 268 will open only so when there is pump pressure available to maintain spool 350 in the shifted position. The flow from line 417 to line 252b can thus be modulated in relation to the pressure on the head end of cylinder 261 and the position of spool 350. This flow will be considerably greater than that which can flow through a small orifice, such as 274 of the FIG. 16 embodiment, while maintaining the regulation and response of the load check valve 268 at a very satisfactory level. The placement of the insert 411 within the passage 252 allows the system to function satisfactorily as a relief valve by means of poppet 276.

Thus, the Applicants have provided a vastly-improved control system wherein a rather low pressure hydraulic system is utilized to operate and control a high-pressure work output system. The invention has been illustrated and described relative to two possible embodiments and it is realized that many other embodiments, modifications, etc., will be obvious to those skilled in the art which do not exceed the purview of the following claims.

What is claimed is:

1. In a directional valve having a passage therein connected to a source of fluid pressure and two controlled ports for connection to a fluid motor, a pilot operated control including at least one check valve means controlling fluid communication between one of said controlled ports and said passage, said check valve means being responsive to pilot fluid pressure changes communicated thereto to connect and disconnect said controlled port and said passage.

each controlled port is also connected to drain through a separate controlled relief valve means, each of said controlled relief valve means being responsive to fluid pilot pressure to change its relief pressure whereby one of said controlled ports can be connected to the passage in communication with the source of fluid pressure and the other controlled port can be relieved to drain at a lower relief pressure for controlling the direction of a fluid motor connected to said controlled ports by appropriate selection of fluid pilot pressures.

l III l l 

1. In a directional valve having a passage therein connected to a source of fluid pressure and two controlled ports for connection to a fluid motor, a pilot operated control including at least one check valve means controlling fluid communication between one of said controlled ports and said passage, said check valve means being responsive to pilot fluid pressure changes communicated thereto to connect and disconnect said controlled port and said passage.
 2. The directional valve defined in claim 1 wherein the pilot operated control includes a second check valve means controlling fluid communication between the passage and the other controlled port, said second check valve means being responsive to pilot fluid pressure changes communicated thereto to connect and disconnect said other controlled port with said passage whereby proper pilot pressure changes will connect one or the other of said controlled ports with said pAssage.
 3. The directional valve defined in claim 1 wherein each controlled port is also connected to drain through a separate controlled relief valve means, each of said controlled relief valve means being responsive to fluid pilot pressure to change its relief pressure whereby one of said controlled ports can be connected to the passage in communication with the source of fluid pressure and the other controlled port can be relieved to drain at a lower relief pressure for controlling the direction of a fluid motor connected to said controlled ports by appropriate selection of fluid pilot pressures. 